Airbus A320. AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING (2016-2023) - page 6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
CFM56 SERIES/SEA LEVEL
STARTING TIME: LESS THAN 60 s
AIR DATA AT AIRCRAFT CONNECTION
80
170
75
160
70
150
65
140
60
130
55
120
50
40
45
50
55
ABSOLUTE PRESSURE (psia)
55
50
45
40
−45
−35
−25
−15
−5
5
15
25
35
45
55
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
120
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
100° C (212° F)
150° C (302° F)
220° C (428° F) MAX.
EXAMPLE:
FOR AN OAT OF 15° C (59° F) AND AN ASU PROVIDING A DISCHARGE TEMPERATURE OF 100° C (212° F)
AT HPGC:
− THE REQUIRED PRESSURE AT HPGC IS 43 psia
− THE REQUIRED AIRFLOW AT A/C CONNECTION IS 66 kg/min.
NOTE:
IN CASE THE ACTUAL DISCHARGE TEMPERATURE OF THE ASU DIFFERS SUBSTANTIALLY FROM THE
ONES GIVEN IN THE CHARTS, A SIMPLE INTERPOLATION (LINEAR) IS SUFFICIENT TO DETERMINE THE
REQUIRED AIR DATA.
N_AC_050500_1_0120101_01_00
Example for Use of the Charts
FIGURE-5-5-0-991-012-A01
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@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
IAE V2500 SERIES/SEA LEVEL
STARTING TIME: LESS THAN 60 s
AIR DATA AT AIRCRAFT CONNECTION
85
180
80
170
75
160
70
150
65
140
60
130
55
120
50
110
45
100
35
40
45
50
55
60
65
ABSOLUTE PRESSURE (psia)
65
60
55
50
45
40
35
−50
−40
−30
−20
−10
0
10
20
30
40
50
60
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
120
140
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
100° C (212° F)
150° C (302° F)
220° C (428° F) MAX.
N_AC_050500_1_0130101_01_00
Engine Starting Pneumatic Requirements
IAE V2500 Series Engine
FIGURE-5-5-0-991-013-A01
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@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
CFM56 SERIES AND CFM LEAP−1A NEO/SEA LEVEL
STARTING TIME: LESS THAN 60 s
AIR DATA AT AIRCRAFT CONNECTION
80
170
75
160
70
150
65
140
60
130
55
120
50
40
45
50
55
ABSOLUTE PRESSURE (psia)
55
50
45
40
−45
−35
−25
−15
−5
5
15
25
35
45
55
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
120
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
100° C (212° F)
150° C (302° F)
220° C (428° F) MAX.
N_AC_050500_1_0140101_01_00
Engine Starting Pneumatic Requirements
CFM56 Series and CFM LEAP-1A NEO Engine
FIGURE-5-5-0-991-014-A01
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5-5-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
PW 1100G NEO/SEA LEVEL
STARTING TIME: LESS THAN 60 s
AIR DATA AT AIRCRAFT CONNECTION
80
170
75
160
70
150
65
140
60
130
55
40
45
50
55
ABSOLUTE PRESSURE (psia)
55
50
45
40
−45
−35
−25
−15
−5
5
15
25
35
45
OUTSIDE AIR TEMPERATURE OAT (° C)
−40
−20
0
20
40
60
80
100
OUTSIDE AIR TEMPERATURE OAT (° F)
ASU DISCHARGE TEMPERATURE:
100° C (212° F)
150° C (302° F)
220° C (428° F) MAX.
N_AC_050500_1_0150101_01_00
Engine Starting Pneumatic Requirements
PW 1100G NEO Engine
FIGURE-5-5-0-991-015-A01
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5-5-0
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AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-6-0
Ground Pneumatic Power Requirements
**ON A/C A320-200 A320neo
Ground Pneumatic Power Requirements
1.
General
This section describes the required performance for the ground equipment to maintain the cabin
temperature at 27 ˚C (80.6 ˚F) for the cooling or 21 ˚C (69.8 ˚F) for heating cases after boarding
(Section 5.7 - steady state), and provides the time needed to cool down or heat up the aircraft cabin
to the required temperature (Section 5.6 - dynamic cases with aircraft empty).
ABBREVIATION
DEFINITION
A/C
Aircraft
AHM
Aircraft Handling Manual
AMM
Aircraft Maintenance Manual
GC
Ground Connection
GSE
Ground Service Equipment
IFE
In-Flight Entertainment
OAT
Outside Air Temperature
PCA
Pre-Conditioned Air
A. The air flow rates and temperature requirements for the GSE, provided in Sections 5.6 and 5.7,
are given at A/C ground connection.
NOTE : The cooling capacity of the equipment (kW) is only indicative and is not sufficient by
itself to ensure the performance (outlet temperature and flow rate combinations are
the requirements needed for ground power). An example of cooling capacity
calculation is given in Section 5.7.
NOTE : The maximum air flow is driven by pressure limitation at the ground connection.
B. For temperatures at ground connection below 2 ˚C (35.6 ˚F) (Subfreezing), the ground
equipment shall be compliant with the Airbus document ”Subfreezing PCA Carts - Compliance
Document for Suppliers” (contact Airbus to obtain this document) defining all the requirements
with which Subfreezing Pre-Conditioning Air equipment must comply to allow its use on Airbus
aircraft. These requirements are in addition to the functional specifications included in the IATA
AHM997.
2.
Ground Pneumatic Power Requirements
This section provides the ground pneumatic power requirements for:
-
Heating (pull up) the cabin, initially at OAT, up to 21 ˚C (69.8 ˚F) (see FIGURE
5-6-0-991-001-A)
-
Cooling (pull down) the cabin, initially at OAT, down to 27 ˚C (80.6 ˚F) (see FIGURE
5-6-0-991-002-A).
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@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
PULL UP PERFORMANCE
1.4
MAXIMUM AIRFLOW
3.0
1.3
1.2
2.5
1.1
1.0
0.9
2.0
0.8
0.7
1.5
0.6
0.5
1.0
0.4
15
30
45
60
75
90
TIME TO HEAT CABIN TO +21° C (+69.8° F) ON GROUND (min)
OAT ISA −38° C ( −36.4° F); GC INLET +70° C (+158° F); EMPTY CABIN; IFE OFF; NO SOLAR
LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
N_AC_050600_1_0010101_01_00
Ground Pneumatic Power Requirements
Heating
FIGURE-5-6-0-991-001-A01
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5-6-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
PULL DOWN PERFORMANCE
1.4
MAXIMUM AIRFLOW
3.0
1.3
1.2
2.5
1.1
1.0
0.9
2.0
0.8
0.7
1.5
0.6
30
45
60
75
90
105
120
TIME TO COOL CABIN TO +27° C (+80.6° F) ON GROUND (min)
OAT ISA +23° C (+73.4° F); GC INLET +2° C (+35.6° F); EMPTY CABIN; IFE OFF; NO SOLAR
LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
OAT ISA +23° C (+73.4° F); GC INLET −10° C (+14° F); EMPTY CABIN; IFE OFF; NO SOLAR
LOAD; LIGHTS ON; GALLEYS OFF; RECIRCULATION FANS ON
N_AC_050600_1_0020101_01_00
Ground Pneumatic Power Requirements
Cooling
FIGURE-5-6-0-991-002-A01
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5-6-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-7-0
Preconditioned Airflow Requirements
**ON A/C A320-200 A320neo
Preconditioned Airflow Requirements
1.
This section provides the preconditioned airflow rate and temperature needed to maintain the cabin
temperature at 27 ˚C (80.6 ˚F) for the cooling or 21 ˚C (69.8 ˚F) for the heating cases.
These settings are not intended to be used for operation (they are not a substitute for the settings
given in the AMM). They are based on theoretical simulations and give the picture of a real steady
state.
The purpose of the air conditioning (cooling) operation (described in the AMM) is to maintain the
cabin temperature below 27 ˚C (80.6 ˚F) during boarding (therefore it is not a steady state).
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@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
COOLING/HEATING PERFORMANCE
1.4
3.0
MAXIMUM AIRFLOW (RECIRCULATION FANS OFF)
1.2
2.5
MAXIMUM AIRFLOW
(RECIRCULATION
FANS ON)
1.0
H
SETTINGS NOT
INTENDED TO BE USED
2.0
C2
FOR OPERATION
C1
0.8
1.5
0.6
1.0
0.4
−10
−5
0
2
5
10
15
20
25
30
35
INLET TEMPERATURE AT GC (° C)
20
30
40
50
60
70
80
90
INLET TEMPERATURE AT GC (° F)
OAT ISA +23° C (73.4° F); EMPTY CABIN; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION
FANS ON; GALLEYS ON
OAT ISA; 164 PAX; IFE ON; LIGHTS ON; SOLAR LOAD; RECIRCULATION FANS ON; GALLEYS ON
OAT ISA −38° C ( −36.4° F); EMPTY CABIN; IFE OFF; LIGHTS ON; NO SOLAR LOAD; RECIRCULATION
FANS ON; GALLEYS OFF
N_AC_050700_1_0030101_01_04
Preconditioned Airflow Requirements
FIGURE-5-7-0-991-003-A01
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5-7-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-8-0
Ground Towing Requirements
**ON A/C A320-200 A320neo
Ground Towing Requirements
1.
This section provides information on aircraft towing.
This aircraft is designed with means for conventional or towbarless towing. Information/procedures
can be found for both in AMM 09.
Status on towbarless towing equipment qualification can be found in ISI 09.11.00001.
One towbar fitting is installed at the front of the leg.
The main landing gears have attachment points for towing or debogging (for details, refer ARM 07).
This section shows the chart to determine the drawbar pull and tow tractor mass requirements as a
function of the following physical characteristics:
-
Aircraft weight,
-
Number of engines at idle,
-
Slope.
The chart is based on the engine type with the highest idle thrust level.
2.
Towbar design guidelines
The aircraft towbar shall comply with the following standards:
-
ISO 8267-1, ”Aircraft - Towbar Attachment Fitting - Interface Requirements - Part 1: Main Line
Aircraft”,
-
SAE AS 1614, ”Main Line Aircraft Towbar Attach Fitting Interface”,
-
SAE ARP 1915, ”Aircraft Towbar”,
-
ISO 9667, ”Aircraft Ground Support Equipment - Towbar - Connection to Aircraft and Tractor”,
-
EN 12312-7, ”Aircraft Ground Support Equipment - Specific Requirements - Part 7: Aircraft
Movement Equipment”,
-
IATA Airport Handling Manual AHM 958, ”Functional Specification for an Aircraft Towbar”.
A conventional type towbar is required which should be equipped with a damping system (to protect
the nose gear against jerks) and with towing shear pins:
-
A traction shear pin calibrated at 9 425 daN (21 188 lbf),
-
A torsion pin calibrated at 826 m.daN (6 092 lbf.ft).
The towing head is designed according to ISO 8267-1, cat. I.
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@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200 A320neo
10
BREAKAWAY RESISTANCE 4%
# OF ENGINES ON FOR PB: 1
ENGINE THRUST 525 daN
70
75
1.5% SLOPE
70
1 ENGINE ON
65
5.8
60
55
5
50
45
10.15
0
0
10
20
30
40
50
60
70
80
0
1
2
0
0.5
1.0
1.5
2.0
TOTAL TRACTION WHEEL LOAD (x 1 000 kg)
No. OF ENGINES
SLOPE ( % )
AT IDLE
EXAMPLE HOW TO DETERMINE THE MASS REQUIREMENT TO TOW A A320 AT 70 000 kg, AT 1.5% SLOPE,
1 ENGINE AT IDLE AND FOR WET TARMAC CONDITIONS:
− ON THE RIGHT HAND SIDE OF THE GRAPH, CHOOSE THE RELEVANT AIRCRAFT WEIGHT (70 000 kg),
− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUIRED SLOPE PERCENTAGE (1.5%),
− FROM THE POINT OBTAINED DRAW A STRAIGHT HORIZONTAL LINE UNTIL No. OF ENGINES AT IDLE = 2,
− FROM THIS POINT DRAW A PARALLEL LINE TO THE REQUESTED No. OF ENGINES (1),
− FROM THIS POINT DRAW A STRAIGHT HORIZONTAL LINE TO THE DRAWBAR PULL AXIS,
− THE Y−COORDINATE OBTAINED IS THE NECESSARY DRAWBAR PULL FOR THE TRACTOR (5 800 kg),
− SEARCH THE INTERSECTION WITH THE "WET CONCRETE" LINE.
THE OBTAINED X−COORDINATE IS THE RECOMMENDED MINIMUM TRACTOR WEIGHT (10 150 kg).
N_AC_050800_1_0010301_01_04
Ground Towing Requirements
FIGURE-5-8-0-991-001-C01
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5-8-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
5-9-0
De-Icing and External Cleaning
**ON A/C A320-200 A320neo
De-Icing and External Cleaning
1.
De-Icing and External Cleaning on Ground
The mobile equipment for aircraft de-icing and external cleaning must be capable of reaching heights
up to approximately 13 m (43 ft).
2.
De-Icing
Wingtip Devices
Wing Top Surface
(Both Inside and
HTP Top Surface
VTP
AIRCRAFT TYPE
(Both Sides)
Outside Surfaces)
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
m2
ft2
A320
100
1 076
2
22
27
291
43
463
A320 Sharklet/neo
100
1 076
10
108
27
291
43
463
Nacelle and Pylon
Fuselage Top Surface
(Top Third - 120˚ Arc)
Total De-Iced Area
AIRCRAFT TYPE
(Top Third - 120˚ Arc)
(All Engines)
m2
ft2
m2
ft2
m2
ft2
A320
138
1 485
24
258
333
3 584
A320 Sharklet/neo
138
1 485
24
258
341
3 670
NOTE : Dimensions are approximate.
3.
External Cleaning
Wing Lower Surface
Wingtip Devices
Wing Top Surface
(Including Flap Track
(Both Inside and
AIRCRAFT TYPE
(Both Sides)
Fairing)
Outside Surfaces)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A320
100
1 076
103
1 109
2
22
A320 Sharklet/neo
100
1 076
103
1 109
10
108
HTP Top Surface
HTP Lower Surface
VTP
AIRCRAFT TYPE
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A320
27
291
27
291
43
463
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5-9-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
HTP Top Surface
HTP Lower Surface
VTP
AIRCRAFT TYPE
(Both Sides)
(Both Sides)
(Both Sides)
m2
ft2
m2
ft2
m2
ft2
A320 Sharklet/neo
27
291
27
291
43
463
Fuselage and
Nacelle and Pylon
Total Cleaned Area
AIRCRAFT TYPE
Belly Fairing
(All Engines)
m2
ft2
m2
ft2
m2
ft2
A320
421
4 532
73
786
796
8 568
A320 Sharklet/neo
421
4 532
73
786
804
8 654
NOTE : Dimensions are approximate.
Page 2
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@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
OPERATING CONDITIONS
6-1-0
Engine Exhaust Velocities and Temperatures
**ON A/C A320-200 A320neo
Engine Exhaust Velocities and Temperatures
**ON A/C A320-200
1.
General
This section provides the estimated engine exhaust efflux velocities and temperatures contours for
Ground Idle, Breakaway and Maximum Take-Off (MTO) conditions.
**ON A/C A320neo
2.
General
This section provides the estimated engine exhaust velocity and temperature contours for MTO,
Breakaway 12% MTO, Breakaway 24% MTO and Ground Idle conditions for the CFM LEAP-1A and
PW 1100G engines.
The MTO data are presented at the maximum thrust rating. The Breakaway data are presented at a
rating that corresponds to the minimum thrust level necessary to start the movement of the A/C
from a static position at its maximum ramp weight. Breakaway thrust corresponds to 12% MTO if
applied on both engines and 24% MTO when applied on a single engine (Idle thrust on the other
engine).
The Idle data, provided by the engine manufacturer, are calculated for operational conditions ISA
+15K (+15˚C), Sea Level, Static and no headwind. In the charts, the longitudinal distances are
measured from the inboard engine core-nozzle exit section. The lateral distances are measured from
the aircraft fuselage centerline.
The effects of on-wing installation are not taken into account. The effects of ground proximity are
not taken into account for PW 1100G engines, but they are taken into account for the CFM
LEAP-1A engines.
The velocity contours are presented at 50 ft/s (15 m/s), 100 ft/s (30 m/s) and 150 ft/s (46 m/s).
The temperature contours are shown at 313K (+40˚C), 323K (+50˚C) and 333K (+60˚C). The
velocity and temperature contours do not take into account possible variations affecting performance,
such as ambient temperature, field elevation or failure cases leading to an abnormal bleed
configuration. To evaluate the impact of these specific variables on the exhaust contours, a specific
study of the airport where the aircraft is intended to operate should be carried out.
Page 1
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6-1-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-1
Engine Exhaust Velocities Contours - Ground Idle Power
**ON A/C A320-200 A320neo
Engine Exhaust Velocities Contours - Ground Idle Power
1.
This section provides engine exhaust velocities contours at ground idle power.
Page 1
May 01/16
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060101_1_0050101_01_01
Engine Exhaust Velocities
Ground Idle Power -- CFM56 Series Engine
FIGURE-6-1-1-991-005-A01
Page 2
May 01/16
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060101_1_0060101_01_00
Engine Exhaust Velocities
Ground Idle Power -- IAE V2500 Series Engine
FIGURE-6-1-1-991-006-A01
Page 3
May 01/16
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060101_1_0110101_01_00
Engine Exhaust Velocities
Ground Idle Power -- CFM LEAP-1A Engine
FIGURE-6-1-1-991-011-A01
Page 4
May 01/16
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060101_1_0120101_01_00
Engine Exhaust Velocities
Ground Idle Power -- PW 1100G Engine
FIGURE-6-1-1-991-012-A01
Page 5
May 01/16
6-1-1
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-2
Engine Exhaust Temperatures Contours - Ground Idle Power
**ON A/C A320-200 A320neo
Engine Exhaust Temperatures Contours - Ground Idle Power
1.
This section provides engine exhaust temperatures contours at ground idle power.
Page 1
May 01/16
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060102_1_0050101_01_01
Engine Exhaust Temperatures
Ground Idle Power -- CFM56 Series Engine
FIGURE-6-1-2-991-005-A01
Page 2
May 01/16
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060102_1_0060101_01_01
Engine Exhaust Temperatures
Ground Idle Power -- IAE V2500 Series Engine
FIGURE-6-1-2-991-006-A01
Page 3
May 01/16
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060102_1_0110101_01_00
Engine Exhaust Temperatures
Ground Idle Power -- CFM LEAP-1A Engine
FIGURE-6-1-2-991-011-A01
Page 4
May 01/16
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060102_1_0120101_01_00
Engine Exhaust Temperatures
Ground Idle Power -- PW 1100G Engine
FIGURE-6-1-2-991-012-A01
Page 5
May 01/16
6-1-2
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-3
Engine Exhaust Velocities Contours - Breakaway Power
**ON A/C A320-200 A320neo
Engine Exhaust Velocities Contours - Breakaway Power
1.
This section provides engine exhaust velocities contours at breakaway power.
Page 1
May 01/16
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060103_1_0030101_01_01
Engine Exhaust Velocities
Breakaway Power -- CFM56 Series Engine
FIGURE-6-1-3-991-003-A01
Page 2
May 01/16
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060103_1_0040101_01_00
Engine Exhaust Velocities
Breakaway Power -- IAE V2500 Series Engine
FIGURE-6-1-3-991-004-A01
Page 3
May 01/16
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060103_1_0130101_01_00
Engine Exhaust Velocities
Breakaway Power 12% MTO -- CFM LEAP-1A Engine
FIGURE-6-1-3-991-013-A01
Page 4
May 01/16
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060103_1_0140101_01_00
Engine Exhaust Velocities
Breakaway Power 12% MTO -- PW 1100G Engine
FIGURE-6-1-3-991-014-A01
Page 5
May 01/16
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060103_1_0150101_01_00
Engine Exhaust Velocities
Breakaway Power 24% MTO -- CFM LEAP-1A Engine
FIGURE-6-1-3-991-015-A01
Page 6
May 01/16
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060103_1_0160101_01_00
Engine Exhaust Velocities
Breakaway Power 24% MTO -- PW 1100G Engine
FIGURE-6-1-3-991-016-A01
Page 7
May 01/16
6-1-3
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-4
Engine Exhaust Temperatures Contours - Breakaway Power
**ON A/C A320-200 A320neo
Engine Exhaust Temperatures Contours - Breakaway Power
1.
This section provides engine exhaust temperatures contours at breakaway power.
Page 1
May 01/16
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060104_1_0030101_01_01
Engine Exhaust Temperatures
Breakaway Power -- CFM56 Series Engine
FIGURE-6-1-4-991-003-A01
Page 2
May 01/16
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060104_1_0040101_01_01
Engine Exhaust Temperatures
Breakaway Power -- IAE V2500 Series Engine
FIGURE-6-1-4-991-004-A01
Page 3
May 01/16
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060104_1_0090101_01_00
Engine Exhaust Temperatures
Breakaway Power 12% MTO - CFM LEAP-1A Engine
FIGURE-6-1-4-991-009-A01
Page 4
May 01/16
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060104_1_0100101_01_00
Engine Exhaust Temperatures
Breakaway Power 12% MTO - PW 1100G Engine
FIGURE-6-1-4-991-010-A01
Page 5
May 01/16
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060104_1_0110101_01_00
Engine Exhaust Temperatures
Breakaway Power 24% MTO - CFM LEAP-1A Engine
FIGURE-6-1-4-991-011-A01
Page 6
May 01/16
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060104_1_0120101_01_00
Engine Exhaust Temperatures
Breakaway Power 24% MTO - PW 1100G Engine
FIGURE-6-1-4-991-012-A01
Page 7
May 01/16
6-1-4
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-5
Engine Exhaust Velocities Contours - Takeoff Power
**ON A/C A320-200 A320neo
Engine Exhaust Velocities Contours - Takeoff Power
1.
This section provides engine exhaust velocities contours at takeoff power.
Page 1
May 01/16
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060105_1_0050101_01_01
Engine Exhaust Velocities
Takeoff Power -- CFM56 Series Engine
FIGURE-6-1-5-991-005-A01
Page 2
May 01/16
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060105_1_0060101_01_01
Engine Exhaust Velocities
Takeoff Power -- IAE V2500 Series Engine
FIGURE-6-1-5-991-006-A01
Page 3
May 01/16
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060105_1_0110101_01_00
Engine Exhaust Velocities
Takeoff Power -- CFM LEAP-1A Engine
FIGURE-6-1-5-991-011-A01
Page 4
May 01/16
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060105_1_0120101_01_00
Engine Exhaust Velocities
Takeoff Power -- PW 1100G Engine
FIGURE-6-1-5-991-012-A01
Page 5
May 01/16
6-1-5
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-1-6
Engine Exhaust Temperatures Contours - Takeoff Power
**ON A/C A320-200 A320neo
Engine Exhaust Temperatures Contours - Takeoff Power
1.
This section provides engine exhaust temperatures contours at takeoff power.
Page 1
May 01/16
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060106_1_0050101_01_01
Engine Exhaust Temperatures
Takeoff Power -- CFM56 Series Engine
FIGURE-6-1-6-991-005-A01
Page 2
May 01/16
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320-200
N_AC_060106_1_0060101_01_00
Engine Exhaust Temperatures
Takeoff Power -- IAE V2500 Series Engine
FIGURE-6-1-6-991-006-A01
Page 3
May 01/16
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060106_1_0110101_01_00
Engine Exhaust Temperatures
Takeoff Power - CFM LEAP-1A Engine
FIGURE-6-1-6-991-011-A01
Page 4
May 01/16
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
**ON A/C A320neo
N_AC_060106_1_0120101_01_00
Engine Exhaust Temperatures
Takeoff Power - PW 1100G Engine
FIGURE-6-1-6-991-012-A01
Page 5
May 01/16
6-1-6
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-0
Danger Areas of Engines
**ON A/C A320-200
Danger Areas of Engines
1.
Danger Areas of the Engines.
Page 1
May 01/16
6-3-0
@A320
AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING
6-3-1
Ground Idle Power
**ON A/C A320-200 A320neo
Ground Idle Power
1.
This section provides danger areas of the engines at ground idle power conditions.
Page 1
May 01/16
6-3-1